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1. The maximum velocity of the Douglas DC-3 (see Figs. 1.33 and 6.80) is 229 mph at an altitude of7500 ft. Calculate the Mach number of the airplane and the pressure sensed by a Pi tot tube on the airplane. 2. The cruising velocity of the Boeing 727 (see Fig. 5 .70) is 610 mph at an altitude of 25,000 ft. Calculate the Mach number of the airplane and the pressure sensed by a tube on the airplane. 3. The maximum velocity of the Lockheed F-104 (see Figs. 1.34 and 5.40) is 1328 mph at an altitude of35,000 ft. Calculate the Mach number of the airplane and the pressure sensed by a tube on the airplane.
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